Title :
Notice of Retraction
Rate-dependent behavior and failure characteristics of carbon/Kevlar hybrid woven composites
Author :
Sung-Choong Woo ; Tae-Won Kim ; Jin-young Kim
Author_Institution :
Survivability Technol. Defense Res. Center, Hanyang Univ., Seoul, South Korea
Abstract :
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Rate-dependent behavior together with failure characteristics of carbon/Kevlar hybrid woven composite under high-strain-rate impact loading were examined. High levels of strain rate, 1008/s~1922/s, tests were conducted on the cylindrical carbon/Kevlar hybrid composite specimen by means of a Split Hopkinson pressure bar (SHPB) and a high pressure gas gun system. The dependence of flow stress on the strain rate was determined firstly. In order to investigate the micro-structural failure mechanisms on the dynamic characteristics of carbon/Kevlar hybrid woven composite, then the fractured zones in the SHPB tests were analyzed by an optical and a scanning electron microscope. According to the high-strain-rate compressive test results, the flow stress at the level of strain 0.01 and peak stress of the materials increased by as much as 52% and 80 % with increasing strain rate over the range of 1008/s to 1922/s. The failure strain, however decreased by approximately 16%. Microscopic examination of the carbon/Kevlar hybrid woven composite showed complicated and multiple growth of various failure mechanisms, such as matrix fracture, fiber/matrix interfacial debonding, yarn-to-yarn friction and wear, fiber breakages including fiber pull-out and fibrillation at the broken fiber tip. Particularly, extensive delamination induced the final fracture of the materials.
Keywords :
carbon; compressive strength; compressive testing; crystal microstructure; delamination; fibre reinforced composites; fracture; friction; high-pressure effects; optical microscopy; plastic flow; scanning electron microscopy; stress-strain relations; wear; woven composites; yarn; C; carbon-Kevlar hybrid woven composites; delamination; fiber-matrix interfacial debonding; flow stress; fracture; high-pressure gas gun system; high-strain-rate compressive testing; high-strain-rate impact loading; microstructural failure mechanisms; optical microscopy; rate-dependent behavior; scanning electron microscopy; split Hopkinson pressure bar; wear; yarn-to-yarn friction; Carbon; Loading; Materials; Strain; Stress; Surface cracks; Weaving; Kevlar; carbon; failure mechanism; high-strain-rate; hybrid composite;
Conference_Titel :
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4799-1014-4
DOI :
10.1109/QR2MSE.2013.6625693